Remote-control system



Oct. 24, 1950 w. 1'. REA 2,527,153

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ATTORNEY which a searchlight may be kept automatically controllable from the control station tot-enabling Patented Oct. 24, 1950 I UNITED STATES 1 PATENT OFFICE i 2,527,153 t REMOTE-CONTROL SYSTEM Wilton '1'; Res, Manhasset, N. Y., assignor to Bell Telephone Laboratories, Incorporated, New York, Y., a corporation of New York Application June 2, 1945, Serial No. 597,204 4 Claims. 343-7) This invention relates to a' searchlight control In accordance with a'rurther i'eatureoi' the insystem and more particularly to a system in vention provision is made in the converter and directed at a target under the control of a radar the control of the searchlight to befiwitche'd until the target approaches within optical range from the radar to the control station softhat a when the radar" or radio direction and range target may be tracked by the radar and the device may be to search for other searchlight maintained trained upon the target distant targets and the direction of the searchby the radar until the target approaches within light may then be controlled under the control optical range, whereupon, in responseto the operof an optical tracker. 10 ation of a switch at the control station the control t h he o e been P p eutomefleof the searchlight may be switched from the radar a y co ol e ec i 0 e Searchlight y a to the control station whereafter the target may radar but it has been found difllcult to accu at y be tracked by optical observation and the searchdh ct ce ta n types 0 archl s and more light maintained trained upon the target by the P r l y those driven by step-byp p control station. The-radar is thus rendered availmotors due to the difficul y n maintaining able for the detection of another target too dismatching errors of the radar and searchlight tanttob detected optically. s ch transmitters as small as the Width of Other features of the invention will become apthe pointe 0f the zero reader meters used at parent upon reference to the following detailed the radar, searchlight and distant control station description when read in connection t t for indicating when the searchlight minted companying drawing in which: at the target being tracked by the radar- Figs. 1 and 2 taken together with Fig. 2 at the It is the Object 0! Present invention right of Fig. l disclose the synchro step-by-step enable a Searchlight be accurately Pointed at converter; Fig. l disclosing in the upper portion an invisible target under the control of a radar ther of the azimuth servo-amplifier and (1156105- until the target is within (Ducal rang? ahd ins in the lower portion thereof the elevation then enable the searchlight beam to be mainrv lifi and Fig 2 showing in the upper tamed directed at the target under the control left portion thereof the azimuth servo-motor and of an optical tracker at the searchlight control Step by step transmitter driven thereby. in the station -lower left portion thereof the elevation servo- In Peordance with one feature of the preseht motor and step-by-step transmitter driven theremvehtlon synchro step'by'step cohverher by and in the right portion thereof the power terposed between the searchlight and the radar. supply equipment for supplying operatingppower The converter receives the error voltage produced to the vacuum tubes of the amplifiers of Fig 1; by the combination of the synchro transmitter Fig. 3 shows schematically in the left portion of the radar and the synchro receiver of the thereof the equipment at the searchlight control searchlight the rientahn the station and in the right portion thereof the radar and searchlight in azimuth fig such searchlight lamp, carbon feeding motor, vent error voltage and applies amp ed error motor and some of the control and indicating m ta g h kg z 2:2 equipment of the searchlight unit; w ch um ves s 9 runs r Fig. 4 shows schematically the remaining equipof a type suitable to drive the step-by-step motor ment of the searchlight unit? which operates thesearchlight in its azimuth Fig 5 Show ch u m i t t movement. The converter also receives the error S 5 y c eh eqh Pmeh. I of a radar unit by which the orientation of the voltage produced by the synchro transmitter 01' searchlight may be controlled to enable an unthe radar and the synchro receiver of the search d ta f th d light in response to the orientation of the radar lingo di 9 mven i h t t and searchlight in elevation, amplifies such error n f d fi 33 0w 2; z voltage and applies the amplified error voltage to z f 3 3 s a armhg drive a second small direct current motor which p e e 058 e mven in turn drives a second step-by-step transmitter S M of a type suitable to operate the step-by-step 8am lg unit motor which tilts the searchlight. These error The searchlight unit disclosed in Fig. 4 and in voltages are those heretofore applied to operate .the right portion otFig. 3 comprises an arc lamp the zero-reader meters at the searchlight control 5. 300, the carbons of which are connected to the station and at the searchlight. positive and negative terminals 30! and 302, and

the feed coil 303 of which is connected through the thermostat 304 between the terminals 301 and 302. Also connected across the terminals 301 and 302 is the ventilatin motor 305, the voltage regulator 306 for the lamp and the armature circuit of the lamp carbon feed motor 308. The shunt field 301 of the motor is connected over terminals of the connector blocks 310 and 311 and over power supply leads 312 and 313, over terminals of connector block 400, over brushes and slip rings, over leads 401 and 402 of the power supply cable and through the ballast resistor 403 to the power supply receptacle 404. The recarbon lamp 315 is lighted over a circuit extending from the positive power lead 402 as traced over a terminal of receptacle 400, over lead 313, through the lamp 315, over switch 314, conductor 316, over switch 405 through the fuse block 406 and thence over power lead 401 of the power supply cable. When the switch 405 is closed the elevation scale lamp 311, the azimuth scale lamp 401 and the meter lamps 408 and 409 are connected in parallel over the fuse block 406 to the leads of the power supply cable whereby such lamps are lighted to illuminat the elevation and azimuth zero-readers 410 and 411, the voltmeter 412 and the ammeter 413.

Voltmeter 412 is connected through the fuse block and over slip rings to the leads 401 and 402 of the power supply cable to indicate the voltage of the power supplied to the Searchlight and the ammeter 413 is connected to the ammeter shunt block 414. Power is supplied from the power cable through the circuit breaker 415, through the recarboning circuit switch 416 and over conductors 318 and 319 to the lamp terminals 301 and 302. A portable lamp 411 is provided which may be plugged up in parallel with the lamp 401.

Two motors are provided for orienting the searchlight in elevation and azimuth. The azimuth motor 418 is located in the base structure of the Searchlight and its rotor shaft is connected through reduction gearing to rotate the upper portion of the searchlight in which the apparatus of the left portion of Fig. 3 and the apparatus disclosed above the slip rings and brushes of Fig. 4 is mounted whereby the searchlight lamp may be turned in azimuth. The elevation motor 419 is mounted in the upper rotatable portion of the Searchlight structure and the rotor shaft is connected through reduction gearing to the horizontal shaft which tilts the searchlight in elevation.

Each of these motors is a multipoled threephase motor with its stator windings positioned mechanically 120 degrees apart. The polarity and magnitude of direct current potentials applied from the brushes of a transmitter of the control station of Fig. 3 or a transmitter of the synchro step-by-step converter of Figs. 1 and 2 produce a rotating field which keeps the motor in a fixed relation with the brushes of the associated transmitter so that the two rotate at the same speed. The stator and rotor windings of motor 418 are connected over terminals of connector blocks 429 and 432 and conductors of cable 433 to contacts of a multiple jack 208 and stator and rotor windings of motor 419 are connected over slip rings and brushes, over terminals of connector blocks 421 and 432 and conductors of cable 433 to other contacts of jack 205.

Two synchro receivers ARs and ERs are provided in the Searchlight assembly. Each of these receivers has a three-windin Y-connected stator and a single rotor winding. The rotor of the azimuth receiver ARs is connected by unity ratio gearing to the vertical shaft driven by the motor 418 which rotates the Searchlight in azimuth and the rotor of the elevation receiver ERa is connected by unity ratio gearing to the horizontal shaft driven by the motor 419 which tilts the searchlight in elevation so that the receiver rotors have the same degrees of movement as the searchlight. The rotor windings of these receivers are connected over slip rings and brushes of the slip ring assemblies 420, 421 and 422 with terminals on the connector block 423 associated with the phase detectors 424A and 424m. The-stator windings are connected to terminals of the connector block 450 which are connected over conductors of cable 434 to contacts of jack 200 whereby they may be connected over the cable 200 terminating in multiple plugs 201 and 202, with the jack 202 connected by the cable 435 with plug 500 which in turn is connectable with the Jack 501 and thence with the synchro transmitters ATR and E'Ia of the radar unit of Fig. 5.

The azimuth and elevation zero-reader meters 410 and 411 are connected over slip rings and brushes of the assembly 422 with other terminals of the connector block 423 associated with the phase detectors 24A and 424s which terminals are multiplied to terminals on the connector block 432 connected over conductors of cable 433, over contacts of Jack 206 and plug 201, over contacts of plu 205 and jack 204, over conductors of cable 324 and with the corresponding zeroreader meters 340 and 341 at the searchlight control station and also in parallel over contacts of plug 203 and jack 202, the conductors of the cable 435 interconnecting the synchro step-bystep converter with the radar unit, and over contacts of the plug 500 and jack 501 with the zeroreader meters 502 and 503 at the radar unit.

Alternating current of volts 60 cycles is supplied to the phase detectors 424A and 4241: from the secondary windings of transformer T2, the primary winding of which is connected to terminals of connector block 423 one of which is connected through a fuse in block 425 to one alternating current output terminal of converter 426 and the other terminal of which is connected overa terminal on connector block 421 with the other alternating current output terminal of converter 426. The direct current terminals of converter 426 are connected over the fuse block 425 and through the voltage regulator 428 to the negative power supply terminal on receptacle 404 and over a terminal on connector block 428 to the positive power supply terminal on receptacle 404. The pilot lamp 430 which is bridged across the alternating current output of the converter 426 is lighted when the converter is functioning properly to produce an alternating current output.

To enable the Searchlight attendant to be signaled from the control station of Fig. 3 a buzzer 431 is provided one terminal of which is connected to the positive power supply terminal of receptacle 404 and the other terminal of which is connected to a terminal of block 432 from which a connection may be made as will be later described to a buzzer key 320 at the Searchlight control station.

Searchlight control station unit The searchlight control station unit is provided with a base portion having connector blocks orientation.

atoms:

32! and 322 totcrminalsmwhichareconnected conductors termlnatinx in theja/ck 323 which may be connected by cable 324 at one endinplugfliinsertablelntoflieiacklhand terminating at the other end in the jack 2!! in which the plug 2!! o! the synchro step-byestep converter unit may be inserted. The termlmls on connector blocks 32l and 322 are connected with brushes of the slip ring assembly 32!. The slip rings of the assembly In: carried by the mtatable upper portion of the crmtrol station rmit and are connected with terminals on the connector block 321.

The upper portion of the control station unit is rotatable in azimuth by a imndwheel 32! and gears 32!! and 33! as schematically illustrated whereby the binoculars 33! are given an azimuth The binoculars are also rotatable in elevation by another handwheel and gearing (not disclosed) whereby they may be kept trained on any distant target.

Rotatable in response to the rotation of the handwheel 328 through gearing (not shown having a suitable step-up ratio, is an azimuth transmitter AT and rotatable in response to the orieni tation of the binoculars in elevation through gearing (not shown). having a suitable step-up ratio, is an elevation transmitter ET. The azi muth transmitter AT has three brushes 332., 333 and 334 which are m positioned 120 degrees apart and are rotatable inside of a segmented circular ring. The circular ring is divided into four 90-degree segments 33!, 336, 331 and 33! each of which comprises a TIS-degree conducting portion and a -degree non-conducting portion. With the switch 33! in the closed position positive potential is connected from terminal 342 of connector block 32! to the oppositely disposed segments 33! and 331 of the ring of transmitter AT and negative potential connected from terminal 344 of connector block 321 to the oppositely disposed segments 33! and 333 of the ring of transmitter AT. Similarly, positive potential is applied from the terminal 343 of connector block 321 to the oppositely disposed segments 345 and 341 of the ring of transmitter ET and negative potential is connected from terminal 344 to the oppositely disposed segments 34! and 34! of the ring of transmitter E1. The brushes of the transmitters AT and ET are connected to terminals on connector block 34! which terminals together with terminals 342 and 343 on connector block 321 are in tin-n connected over slip rings and brushes of the asembly 32! to terminals on the connector block 32l which, in turn, are connected to contacts oi the multiple jack 323. As before stated, the jack 323 is connected by the cable 324 and over jack 2!! to the synchro step-by-step converter whereby, as hereinafter described, the brushes and ts oi the transmitters may be connected with the stator and rotor windings of the motors 4]! and 4|! of the Searchlight. v

The zero-reader meters 34! and 3 are connected to terminals on the connector block 322 which terminals are in turn connected over slip rings and brushes of the 32! with terminals on the connector block 322 whereby, as previously described, they may be connected in parallel with the zero-reader meters of the searchlight and radar rmits and to the phase detectors 424A and 424:. Imilluminatim the zero-reader meters a lamp 3!! is provided the circuit for which may be closed by the switch 3Il the negative powaterminal 344.

For purposes a burner is providedwhich. when operated, a v wacircuitfromthenegativepowerterminal 34! to the 352 on connector block 321, over :a slip ringandbmshofylfltoatermmalon connector block 322, thence over contacts of Jack 323 and plug 32!, a conductor of cable 324, contacts oi Jack 2!! and plug 2 contacts of plug 231 and jack 2!!, and thence as previously described through the buzzer 431 at the searchlight unitto positive power supply terminal on receptacle 531 Key 32! also controls the closure of a parallel circuit extending over contacts of plug 2!3 and jack 2!2 and contacts of plug 5!! and jack ill through the buzzer 531 at the radar "unit of Hgw 5 Radar control unit The radar unit shown schematically in Fig. 5 comprises an antenna assembly 534 consisting chiefly of four of coaxially .1 ed antenna radiators or dipoles SIS; a main reflector 5!! for the electromagnetic beam, a lobe switcher or mechaniml rotating switch 531 for the phase of the voltages among the dipoles by a change of capacity thus shifting the direction of the, a square wave magneto type generator 5!! and a direct current motor 5!! which drives both the lobe switcher and the generator. The lobe switcher in combination with the .symmetnimliy located dipoles causes the electnotic beam to rotate comically about its axis at an angle of about 4 degrees. The beam is actually shifted in four steps, first to the right, then down, then to the left and then up. A smaller auxiliary reflector BI! is located immediately in front of the main reflector to a better field pattern. The square wave generator 5!! establishes the basic timing interval for synchronizing all of the radar functions including exact time at which outgoing pulses are transmitted and the conhol of the displays on the oscilloscope.

For transmitting the position of of theantennatothesearchlightrmitofl igs. 3and 4 so that the searchlight may be elevated to the same position, the elevation synchro transmitter E'la is suitably connected by gearing to shaft by which the antenna is tilted in elevation The stator windings of this transmitter are connected over slip rings and brushes of the assembly 5 which is interposed between the antenna assembly and the drive unit indicated by the box 312, with contacts of the jack 5!! which in turn "is connected by contacts of plug ill, conductors of cable 435, contacts oi -jack 2!2, contacts of plugs 2!3 and 2", contacts of jack 2!! and conductors of cable 434 to terminals on connector block 35! and thence to the stator windings of the .synchro receiver ERs of the Searchlight. The rotor ing of the transmitter ET}; is also connected over gsotherslipringsandbnlshmoftheassemblyilt toconhlctsofjsckill whichinturnareconnectedby contacts of plug 5!!, conductms of cable 435, contacts of jack 2!2, contacts of plugs 2!3 and 2",, contacts of jack 2!! and cmductors oicable434toterminalsonconnectorblock4fl t1omtedbctweenflreantennaassemandthencetothem-cyclealternatingcunent outgutofthecrmvertm-flIoftheseamhlight uni Thedriveunit l2 comprisesthe bly I and the transmitter unit "3. This equipment includes a ring gear mounted on the mast I23, driven through a reduction gear box 5 from an azimuth control wheel 5|! in the control unit 5!! by which the antenna may be directed in azimuth. The drive unit also comprises mechanism (not shown) by which the antenna assembly may be tilted in elevation. This mechanism is driven through the reduction gear box 5!! from a control wheel Ill in the control unit 5.

A synchro transmitter ATa is suitably geared to the mast 523 for transmitting the position of azimuth of the antenna to the Searchlight unit of Figs. 3 and 4 so that the searchlight may be rotated in azimuth to the same position. The stator windings of this transmitter are connected over contacts of jack 5M and plug 530, conductors of cable 435, contacts of jack 202, contacts of plugs 233 and 2", contacts of jack 2" and conductors of cable 434 to terminals on connector block 353 and thence to stator windings of the synchro receiver ARs of the searchlight unit. The rotor winding of the transmitter ATa is connected in parallel with the rotor winding of transmitter E'Ia over the circuit previously described to the 60-cycle alternating current output terminals of the converter 42' at the Searchlight unit.

The coaxial transmission line 52! is located within the rotatable mast 520 and provides a connection between the antenna assembly 505 and the transmitter-receiver unit H3. The transmitter-receiver unit 5|3 consists of a receiver unit 522, a transmitter unit 523, and a transmit-receiver box 524. Direct current impulses which are precisely timed and produced jointly by the square wave generator 508 and at indicator unit 525 are amplified to a high voltage in the amplifiers comprising the modulator unit 525 and are then impressed on the magnetron cathode causing the magnetron 523 to oscillate at an ultra-high frequency for most of the duration of the pulse. The short spurts of ultra-high frequency radio energy are transmitted through the coaxial transmission line 52| past the T-R box 524 and thence to the antenna dipoles 535.

The T-R box 524 is a high speed switching device which is arranged to separate the receiver 522 from the coaxial transmission line when the intense impulses are being transmitted.

The radio frequency receiver 522 uses resonant cavity type amplifiers 521 to provide two stages of amplification of the ultra-high frequency echo signals. The amplified ultra-high frequency pulses are then passed to a resonant cavity type modulator 528 together with a beat frequency which is adjustable to be 60 megacycles below the incoming radio frequency signals. The modulator converts the incoming radio frequencies to a (SO-megacycle intermediate frequency. The beat frequency is generated by a resonant cavity type oscillator 529 located in the indicator unit 525.

The modulator unit 526 receives triggering pulses from the synchronizing or timing unit 530 tion. The air unit produces high voltage impulses. shapes the impulses and regulates their duration. The oil unit has a high voltage rectifier and voltage doubler to generate a positive 20- kilovolt supply used in conjunction with two pulse amplifiers which are driven by the pulses generated in the air unit. The output of the pulse amplifiers of the oil unit is delivered to the magnetron of the transmitter unit 523.

The indicator unit provides in a central location practically all of the electrical controls and indicators for operating the radar system. These include three oscilloscopes: a range oscilloscope 53l for indicating range; an azimuth oscilloscope 532 to provide indications for controlling the direction of the antenna in azimuth and an elevation oscilloscope 533 to provide indications for controlling the direction of the antenna in elevation.

The indicator unit has three principal functions which are performed by vacuum tubes and their associated circuits. These functions are:

' to provide basic timing intervals synchronized of the indicator unit 525 and generates high with the position of the electromagnetic beam; to furnish appropriately timed horizontal sweeps on the oscilloscopes and to unblank the cathode ray oscilloscopes at the proper intervals to display the target indications correctly; and to convert all incoming echo signals within the range of the radar system to a series of vertical deflections arising at scaled intervals on the range screen and to display those particular echo signals which are selected by the manually-set position of the range notch as vertical parallel pips on the azimuth and elevation oscilloscope screens.

As previously stated one unit of this equipment is the synchronizing or timing unit 530. The intermediate frequency amplifier 534 is a fourstage amplifier which receives the output from the receiver unit 522 and applies its amplified output upon the video amplifier 535. The video amplifier and gain control block 535 represent the equipment required for displaying vertical defiections on the screens of the oscilloscopes. The oscilloscopes are normally blanked out (no screen spots) and are unblanked only for the duration of a sweep. The sweep and unblanking functions, represented by the block 535, control the display of the horizontal sweep in the three oscilloscopes with respect to their initial starting periods, their lengths and their speeds.

As previously stated the indicator unit is also provided with zero-reader meters 502 and 503 for indicating to the radar operator when the Searchlight has been oriented in azimuth and elevation positions corresponding to the direction of the radio beam. The buzzer 531 is also provided whereby the radio operator may be signaled from the searchlight control station.

Power is supplied to the radar equipment from the Searchlight over a cable 436 extending from the power supply receptacle 304 at the searchlight to the motor generator unit 538. The direct current motor of the unit 538 is operated by power delivered over the cable 436 and drives a 27-volt direct current generator and a to -volt 400-cycle alternating current generator. The generated power is supplied to the power distribution unit 539 from which power is supplied to the power supply unit 540 of the transmitter-receiver, to power supply units 5 and 542 of the modulator unit 526, and to power supply unit 533 of the indicator unit 525, to the blower motor 5 and over a slip ring and brush of the slip ring assembly III to the motor assigns Sunchro step-bu-step converter The synchro step-by-step converter shown in Figs. 1 and 2 serves to amplify the error voltages applied by the phase detectors 424A and 424s of the searchlight to the zero-reader meters resulting from the out-of-phase setting of the searchlight with respect to the setting of the radar antenna.

The-converter is provided with two substantially identical servo-amplifiers disclosed in detail in Fig. 1, motor control relays AA, Ba, Ar: and Br: operable from the outputs of the amplifiers, direct current servo-motors MA and Mn controlled by the control relays, transmitters TA and Tr: driven by the motors MA and Ma, respectively, power supply equipment including the tubes VTI to'VTl, inclusive, shown in the right portion of Fig. 2. and control relays 200 to 2, inclusive.

The azimuth servo-amplifier disclosed in the upper portion of Fig. 1 is of the type fully disclosed in the application of B. Ostendorf, Jr., Serial No. 597,205 filed concurrently herewith which matured into Patent No. 2,472,611 issued June 7, 1949. The amplifier is responsive to a non-grounded pulsating control signal or error voltage applied across the input terminals I M and I02 which are positive or negative only with respect to each other. A positive voltage on terminal IOI with respect to terminal I02 can exist, or conversely a positive voltage on terminal I02 with respect to terminal IOI can occur. The polarity of the voltage determines whether the motor Ma will rotate in a clockwise or in a counter-clockwise direction and the amplitude of the voltage determines the relative speed at which the motor will run. Normally the input terminals MI .and I02 are interconnected over conductors I03 and I04 and the upper back contact of relay 209, but when relay 209 is operated the pulsating error voltage is applied across terminals IOI and I 02 from the azimuth phase detector 4241i 01' the searchlight unit over conductors 431 and 438 connected at the connector block 432 to conductors of cable 423 which, in turn, are connected over contacts of Jack 200 and plug 201, conductor 2|! and conductor I03 to terminal IN, and conductor 2I0, upper front contact 01 relay 209 and conductor I04 to terminal I02.

The pulsating error voltage supplied between the terminals IOI and I02 is filtered by the lowpass ladder type filter comprising the series-connected choke coils LI and "L3, L2 and L4, and bridged condensers CI to C5, inclusive. The impedance of the filter matches the load impedance of 39,000 ohms (resistors R26 and R40) connected to the grid terminals of they twin triode amplifier tube VT8.

The double-resistor, double-capacitor bridge consisting of resistances RH and RI 8, and condensers CIA and CIB balances out any spurious alternating current or direct current voltages leaking to terminals MI and I02 or induced thereon. This is necessary because of the high gain amplification following. The condenser bridge is a low impedance shunt for extraneous high frequency voltages. The center tap of the bridge connects to the isolated O-V reference nected to the O-V bus bar balances out any ex- 10 bus bar of. the servo-amplifier. This establishes an arbitrary reference for the error voltages which are applied across the terminals IN and I02. Thus with respect to other apparatus components oi the amplifier one-half of the eflectivev error voltage is positiveor negative on one terminal as compared with the opposite polarity on the other terminal of the pair.

The double condenser bridge comprising condensers C4 and C5 with the center tap also contraneous longitudinal voltage which may be present on the input terminals MI and I02.

The twin triode equalizer tube VTI has its control electrodes connected to the output conductors I05 and I 06 of the filter section of the amplifier through condensers C24 and C I 9, respectively,

. and through resistors R22 and R44 with the O-V bus bar. Tube VTI also has its cathode connected through the resistances R2I and R43 to the O-V bus bar. Plate potentials for the tube W! are supplied through the voltage dividers comprising'resistorsRH and R24 for the plate of the upper unit and resistors R45 and R46 for the plate of the lower unit. One end of each of these voltage dividers is connected to the O-V bus bar and the other end of each divider is connected to the +I50-V bus bar. Any 400-cycle alternating current hum which is superimposed in the output of tube VTI is thus reduced insignal strength as regards the control grids of the succeeding amplifler'tube VT8 in the ratio of 27,000 ohms to 147,000 ohms. This reduction in alternating current hum is accomplished without sacrificing gain in the equilizer tube VTI. The plates of tube VTI are connected with the grids of the succeeding amplifier tube VT8 through the condensers C20 and C25.

The relative importance of the equalizer tube can be better understood if it is realized that the servo-amplifier could be operated with the tube removed from the socket. However, the tube adds a very desirable operating feature, namely that of increasing the effect of error voltage changes. This is of particular importance in connection with an error voltage change resulting from stopping or changing the direction of the control wheel 5I0 of an associated radar. A quick efiective braking oi the control circuit prevents the motor Ma and the Searchlight which is controlled by the motor from overrunning or overshooting.

The necessity for servo accuracy requires the use of a high gain amplifier which, of course, tends to offer the basic condition for producing electromechanical oscillations. In the event of a tendency to oscillate, the equalizer tube VTI enables the'mechanism to more rapidly recognize a change in the rate of motion. This tends to prevent it from overshooting through zero, then reversing its direction and coasting back past zero and continuing to do this thus setting up a "hunt" or oscillation.

Tube VT'I provides a class A amplifier having a rising gain versus frequency characteristic. The voltage gain, is zero at zero cycles, about 7 at 5 cycles and rises to 10 at frequencies higher than 20 cycles. Accordingly there is no circuit function performed by the tube if the radar control wheel 5? is operated at a slow or at a very gradually accelerated rate.

The manner in which the equalizer tube functions is illustrated by, the following example.- It will be assumed that a positive error voltage changing in a positive direction exists on terminal llil with respect to terminal I02. A positive direct current bias is placed on the control grid of the lower unit of tube VT8 whereas a negative voltage is impressed on the control grid of the lower unit of tube VT1. The output of the lower unit of tube VT1 is therefore in a positive direction. This positive voltage is connected to the control grid of the lower umt of tube VT8 to reenforce the error voltage rather than to oppose it. It can readily be shown that a similar correspondence in polarity exists between the error voltage and the output voltage of the upper unit of tube VT1 and that the voltages join, to bias the grid of the upper unit of amplifier tube VT8.

It can be stated therefore that a change in error voltage produces a changing direct current component which places the equalizer tube VT1 in operation to magnify the signal voltage change and connect it to the succeeding amplifier stage.

The dual triode amplifier tubes VT8 and VT9 provide a two-stage high gain class A direct cur-' rent amplifier. Tube VT8 has an amplification factor of about 70 to 1 and employs a high plate load resistance comprising resistors R28 and R50. A condenser-resistance filter is provided in the in put leads of tube VT9 to reduce further any residual 400-cycle alternating current hum which may have passed the amplifier tube VT8. These filters comprise the resistor-condenser combinations R29-C2l and Rl---C25.-

The cathode resistor network associated with the tube VT8 produces a bias of about 1.5 volts and includes a screwdriver adjustable potentiometer R68 to permit the balancing of the tube operation by offsetting resistance variations of the apparatus. The resistance network includes the potentiometer R68 connected between the cathodes of the two units of tube VT8 connected in parallel with the series-connected equal resistances R66 and R51, the junction point between which latter resistors is connected to the slider of potentiometer R68 and through resistance R65 to the +150-V bus bar, and resistors R and R41 which connect the cathodes of the tube to the O-V bus bar.

The cathode resistor R30 which is common to the two cathodes of the twin triode amplifier tube VTB provides stabilized bias for such tube. Tube VT! is directly coupled to the output of tube VT8 through the coupling resistors R29 and RSI and is connected in push-pull circuit to reduce longitudinal voltages arising from the variations in the preceding stages.

As in the case of the equalizer tube VT1, the servo-amplifier would operate even if the clutch tube VTHl were removed from its socket. However, the tube slows down the effect of those sudden large voltage changes which tend to cause the motor to rotate but does not effect changes which result in stopping the rotation of the motor. A sudden large error voltage may be presented to the amplifier when the servo-amplifier is switched into connection with the radar after a period of idleness or if a handwheel of the radar is jerked rather than moved at a uniform rate of speed. The clutch tube, a twin diode, temporarily short circuits any incoming positive error voltages. This condition lasts only during the brief period while either condenser C22 or condenser C21 is charging. Thus the tube tends to moderate extremely large error voltages by presenting them somewhat more gradually to the 'multivibrator tube, but it introduces no delay in braking the circuit.

Amplifier tube VTQ is directly coupled to the multivibrator tube VTI I. The coupling between the upper units of these tubes comprises the voltage divider including resistors R3l, R33, R35 and R33 connected in series between the +450-V bus bar and the O-V bus bar, the plate of the upper unit of tube VT! being connected to the junction point between resistors R1 and R33 and the grid of tube VTH being connected to the junction point between resistors R35 and R35. The coupling between the lower units of these tubes comprises the voltage divider including resistors R53, R55, R51 and R58 connected in series between the +450-V bus bar and the O-V bus bar, the plate of the lower unit of tube VT9 being connected to the junction point between resistors R53 and R55 and the grid of tube VTH bein connected to the junction point between resistors R51 and R58.

The twin diode clutch tube VTIO shunts only those voltage outputs of the amplifier tube VT9 which change in a positive direction. Due to the polarity relations of the circuit only one unit of tube VTIO conducts at any instant. To accomplish this the plates of amplifier tube VTB are interconnected through the two resistors R32 and R54, the junction point between which resistors is connected through other resistors R34 and R56 with the cathodes of tube VTIII. The cathode of the upper unit of tube VTIO is also connected through the condenser C22 to the junction point between resistors R33 and R35 and the cathode of the lower unit of tube V'IIO is connected through condenser C21 to the junction point between resistors R55 and R51. The plate of the upper unit of tube VTHI is connected to the plate of the lower unit of tube VTB and the plate of the lower unit of tube V'IIfl is connected to the plate of the upper unit VT9. The shunted positive voltage produced in one unit of the tube VTI 0 is superimposed on one grid of the multivibrator tube VTH but in a direction opposite to that of the normal signal output from the amplifier tube VT! and accordingly decreases the net difference otherwise existing between the two grids of the multivibrator tube VT! 1. Assuming that an error voltage at a particular instant is changing in a positive direction on the terminal I01, while it is changing correspondingly in a negative direction on terminal I02 then the polarity relations of the voltage conditions in the servo-amplifier circuit are as shown in the following table:

Direction of voltage changes It may be noted from the above table that the output voltages on the plates of the multivibrator tube VTH will differ in peak values by amounts which are less than would result from the effect of error voltages alone due to the action of the clutch tube VTID. In other words the unbalance of the circuit is temporarily lessened. The shuntthe circuit for stopping the motor.

The dual multivibrator tube VTII has .symmetrical feedback circuits for each of its two units. Under balanced operating conditions during which both grid bias voltages are equal, the multivibrator oscillates to produce approximately balanced square waves at its plate terminals, the

waves alternating at a frequency of about 40 cycles per second with approximately equal open" and closed periods. The output from one plate is the inverted counterpart of the output from the other plate. This relationship results from the symmetrical circuit condition wherein the frequency of oscillation and the relation of the periods are established by the constants of the two resistor-condenser feedback circuits. One of thesecircuits includes the resistor R31 connected in series with condenser C28 between the plate of the upper unit of the tube and the grid of the lower unit. The other of these circuits includes the resistor R59 connected in series with condenser C23 between the plate of the lower unit of the tube and the grid of the upper unit. As before stated, the grids of the tube are also connected through resistors to the plates of the amplifier tube VTS."

The cathodes of the tube VTII are connected to the +150-V bus bar and plate potential from the +450-V bus bar is supplied to the plate of the upper unit through serially connected resistances R31 and R38 and to the plate of the lower unit through serially connected resistances R59 and R60. If the signal voltages impressed on the two grids of tube VTI ishould become unequal, then the periods of the square waves would become unequal. The time at which one unit of the multivibrator tube cuts off or again conducts then depends not only upon the resistor-condenser time constant of the circuit but also on the level of potential toward which the circuit tends to charge. For example with a given resistor-condenser circuit and a fixed starting voltage, it will take a longer time for the circuit to charge to a potential resulting in tube conduction if the charging cycle approaches a lower rather than a higher voltage on the grid.

It will be remembered from the preceding discussion that the various components of the servoamplifier are balanced under operating conditions only when the servo-motor controlled searchlight and the radar are oriented in exactly the same direction since then no error voltage is impressed across the terminals I! and I02. At all other times unbalanced voltages occur, the polarities and magnitudes of which vary depending upon the direction and amount that the radar and ,searchlight are out of phase. It unbalanced voltages are eventually connected to the grids of the two units of multivibrator tube VTH, the unbalanced voltages cause one unit to take a longer time to cut in than the other, thus producing unbalanced square waves as an output. The progression of the unbalanced periods of the waves in a positive or negative direction depends upon the d rection in which the searchlight departs from the radar and the relative duration of the periods are approximately proportional to the ma nitude of the out of phase relationship.

The multivibrator tube VTII is coupled with the dual triode bufler tube VTI2 which functions as a power amplifier. The plate of the upper unit of tube VTH is coupled with the grid of the upper unit of tube VTI! through resistor R39 which is included in the voltage divider extending from the +450-V bus bar through the serially connected resistors R38, R31, R39 and R40 to the O-V bus bar. The plate of the lower unit of tube VTI I is coupled with the grid of the lower unit of tube VTIZ through resistor ROI which is included in the voltage divider extending from the +450-V bus bar through the serially connected resistors R60, R59, RBI and R62 to the O-V bus bar.

The two outputs of the buffer tube VTI! operate two control relays AA and BA which jointly cause the motor MA to-rotate in a clockwise or a counter-clockwise direction and at varying speeds. The plate of the upper unit of tube VTI 2 is connected through resistor R, over conductor I01 and through the winding of relay AA to the +450-V bus bar and the plate of the lower unit of the tube VT|2 is connected through resistor R63,-over conductor I08 and through the winding of relay Bx tothe +450-V bus bar. Condenser C62 provides a shunt across the winding of relay- AA to absorb the inductive disturbances arising from the operation andthe release of the relay and condenser C63 performs a similar function in connection with relay BA. An important function of the buffer tube is to separate the relays electrically from the multivibrator circuit so that inductive disturbances arising from the operation of the relays will not produce adverse effects in the multivibrator operation.

The relays AA and BA are preferably of the mercury contact type such as is disclosed in the application of E. T. Burton Serial No. 545, 985, filed July 21, 1944, which issued January 18, 1949 as Patent No. 2,459,306 but relays of other types could be used, provided they are fast in operation, sensitive and are capable of handling a considerable contact load. Each of these relays comprises an envelope of glass or other suitable ma- I terial through the bottom of which an armature terminal is sealed and through the top of which two other terminals are sealed. Secured to the inner end of one of the upper terminals is a front contact of m'asnetiematerial and secured to the inner end of the other upper terminal is a back contact of non-magnetic material. Secured to the lower terminal by a reed is an armature of magnetic material biased against the backcontact and attractable toward the front contact. A pool of mercury is placed in the bottom of the envelope from which mercury is conducted to the contacts-by wick action. Surrounding the en-, velope is an operating coil or winding which when energized sets up a flow ofmagnetic fiux through the armaturer and front contact to cause the movement of the armature towards the front contact.

The motor MA has its field FA connected across supply conductors 2H and M8 and through contacts of switch 2|! to which a source of 24 volts direct current is connected from the radar as previously described. The armature circuit of the motor is connected between the swing contacts of the relay through the choke coil Ll5 paralleled by resistance R10 to limit the alternating component of the current in the motor armature and to serve to smooth the operation of the motor. The choke coil LIB paralleled by resistor R69 is included in the connection from supply conductor 2H to the front contacts of the relays to minimize contact deterioration during the brief periods when a contact transfer occurs in either relay and all the contacts are in engagement. A network of resistors and condensers is provided for protecting the contacts of the relays. For example, the swing and front contact of relay AA are bridged by the series combination of resistor R1! and condenser C39A and also a bridge consisting of resistor R14 in series with a parallel combination involving resistor R15 and condenser C. These bridges are separated by an inductive resistor R13. Similar networks are-provided for protecting the swing and front contact of relay AA, the swing and front contact of relay BA and the swing and back contact of relay BA.

The association of the two control relays AA and BA with the multivibrator and buffer tube previously described provides an arrangement whereby one relay is operated while the other is released. The relays operate in this manner at a rate of about 40 cycles per second. If the servo-amplifier is in a balanced condition, that is, no error voltage is applied across the terminals i! and I02. symmetrical square waves are produced at the outputs of the buffer tube VTI2 and the relays AA and BA alternately operate and release in response to the essentially square waves but in an opposite order.

Accordingly with relay AA operated and relay BA released, current will flow from conductor 2 l1 of the power supply through the resistor R69 in parallel with choke coil LI 3, through resistor R13, over the front contact of relay AA, through resistor R in'parallel with choke coil Ll5, through the armature circuit of motor MA, over the back contact of relay BA and through resistor R16 to conductor 218 of the power supply. When relay BA is operated and relay AA is released, current will flow from conductor 2|1 of the power supply through resistor R59 in parallel with choke coil LE3. through resistor R11, over the front contact of relay BA, through the armature circuit of motor MA, through the resistor R10 in parallel with choke coil Li5, over the back contact of relay AA and through resistor R12 to conductor 218 of the power supply. These impulses of power are equal and are transmitted alternately in opposite directions through the armature circuit of the motor and accordingly the net direct current voltage connected across the armature circuit of the motor is zero and the motor remains at rest. However, the armature will vibrate sufficiently to overcome the static friction of the motor enabling the motor to rotate smoothly at very low speed.

If unbalanced voltage conditions exist, resulting for example in relay AA remaining in its front contact closure position for a longer time in any given interval than it remains in its back contact closure position and at the same time, relay BA remains in its back contact closure position for a longer time than it remains in its front contact closure position, the impulse of power transmitted through the armature circuit of the motor MA, when relay AA is operated and relay BA is released, will be lengthened and the impulse of power transmitted in the opposite direction through the armature circuit of the motor when relay AA is released and relay BA is operated will be shortened and the net voltage across the armature circuit of the motor will cause the motor to turn in one direction of rotation. This net effective voltage will, of course, govern the speed of rotation. A higher net voltage results if the closed periods for operating one of the relays greatly exceed in duration the open periods in which the relay is released.

The azimuth motor MA drives the transmitter TA through the gear box 220 which has a reduction gear ratio of 25 to 1. The transmitter is of the same type as the transmitters AT and ET of the searchlight control station previously described. The brushes of the transmitter are interconnected by the bridging condensers C55, C56 and CS1 to reduce sparking when a brush passes from a conducting to a non-conducting segment and four current limiting resistors R90, R8], R82 and R93 are connected between the brushes and the positive potential segments 22! and 223 of the transmitter and the front contacts of relay 2| l.

The motor MA also drives the friction-operated switch 225. This switch comprises two semicircular segments 226 and 221 having grooved peripheries and mounted on the shaft which drives the brushes of the transmitter TA and held in frictional engagement with such shaft by a spiral spring 228 disposed in the grooves of the segments 226 and 221. Secured to the segment 226 and insulated therefrom is a switch arm 229 the free end of which is mounted for movement between two fixed contacts which are connected to the ends of a resistance bridge comprising resistors R18 and R19. The junction point of the bridge may be connected over one contact of the azimuth lead switch 230, over conductor 29l and through resistor RH with the output conductor I05 of the filter section of the azimuth servo-amplifier and the switch arm 229 is connected over another contact of switch 239, over conductor 232 and through resistor RI2 with the output conductor I06 of such filter section.

For supplying potential across the bridge consisting of resistors R18 and R19, shunted by condenser Cl9, the lead voltage rectifier tube VTG is provided. This tube is a twin diode having its two plates connected together and to one terminal of the secondary winding S6 of power transformer TI and having its cathodes also connected together and to one terminal of the resistance bridge and having its filament heated by current supplied from the secondary winding S8. The lower terminal of the secondary winding is connected to the other terminal of the resistance bridge. The tube VTG thus rectifles the 6.4-volt, 400-cycle alternating current applied to the secondary winding S6 of the transformer and applies such rectified current across the resistance bridge whereby the junction point between the resistors R18 and R19 is negative with respect to the outside terminal of resistor R19 and is positive with respect to the outside terminal of resistor R19.

The movement of the switch arm 229, through the frictional driving connection with the shaft of transmitter TA with either of its fixed contacts, provides a means for connecting a predetermined value of voltage as determined in value by the rectifier tube VTB and bridge resistors R18 and R19, over the contacts of the lead switch 230, conductors 23| and 232 to conductors I05 and I06 of the azimuth servo-amplifier which accentuates the error voltage to cause the motor-driven transmitter TA to advance further than it otherwise would. This lead tends to offset inherent lag in the searchlight driving system.

The fixed error voltage is normally disconnected from conductors HI and 232 at the contacts of switch 225. The switch arm is ar- 7 ranged so that the lower fixed contact is engaged when the motor revolves in one direction whereas the upper fixed contact is engaged when the motor revolves in thegopposite direction. Keeping in mind this arrangement and the polarities of the non-grounded rectifier tube VT3 output voltage with respect to the junction point between resistors R10 and R19, it may be noted that if voltage is connected through the lower fixed contact of switch 225 to con ductor 232, this voltage is negative with respect to that connected to conductor 23I. On the other hand, if voltage is connected through the upper fixed contact of switch 225 to conducton 232, this voltage is positive with respect to that connected to conductor 23!.

The elevation servo-amplifier shown in the lower portion of Fig. 1, the relays A1; and Ba, the servo-motor Mn and the transmitter Tn controlled by the amplifier, are identical in structure and function with the similar elements of the azimuth servo-amplifier just described except that the lead switch 225 and connections therefrom to the input of the servo-amplifier are omitted since tilting of the Searchlight in elevation tends to be done more gradually than rotation in azimuth and inherent delays in the elevation searchlight control system are therefore of less significance. Normally the input terminals I 5i and I52 of the elevation servoamplifier are interconnected over conductors I53 and I 54 and the upper inner back contact of relay 209 but when relay 209 is operated the pulsating error voltage is applied across the terminals I5I and I52 from the elevation phase detector 424:; of the searchlig'ht unit over conductors 433 and connected at the connector block 432 to conductors of cable 433 which in turn are'connected over contacts of jack 200 and plug 201, conductor 233 and conductor I54 to terminal I52, and over conductor 234, over the inner upper front contact of relay 209 and over conductor I53 to the terminal II.

Power for operating the tubes of the servoampllfiers is provided by the equipment shown in the right portion of Fig. 2. Power of 400 cycles at 115 volts is secured from the motor generator unit 530 of the radar unit as .previously described and is transmitted over contacts of jack SM and plug 500, conductors of cable 435, contacts of jack 202 and plug 203,

and over contacts of switch 2| 9 through the primary winding PI of the power transformer TI. Heating supply current is supplied to the filaments of tubes VTI, VTB, VTO, VTII and VTI2 of the azimuth servo-amplifier and to the filaments of tubes VTI3, VT, VTI5, VTI! and VTIl of the elevation servo-amplifier over conductors 235 and 238 from the secondary winding SI of transformer TI. Heater supply current is applied through the filaments oi tubes VTIO and VTI3 over conductors 231 and 233 from the secondary winding 82 of transformer TI.

For supplying +300 volts between the +450-V and +150-V :bus bars the full wave rectifier tube VTI is provided, the filament oLwhich is heated by current from the secondary winding S3 of the transformer TI. 84 of transformer Tl supplies 400-cycle 400-volt alternating current to the plates of tube VTI,

the mid-point terminal of the winding connected to the +150-V bus bar.

The rectified output 01 tube VTI is smoothed S4 being by a filter consisting of the series choke coil L3 and the bridged condensers CH and CH and is I regulated at a potential of about +300 volts with Secondary winding a n winding S5 of the transformer.

respect to the +-V bus bar connected to the center tap of the secondary winding S4 of transformer TI. This regulation is accomplished by vacuum tubes VT3 and VT4. The pentode tube VT3 serves as a variable impedance connected in series between the output of tube VTI and the +450-V bus bar. The value of the impedance in series with the output depends upon the plate-cathode current of tube VT3 which in turn is changed by the potential connected to the control grid of the same tube. The control grid is influenced by the voltage drop across resistance R3, 9. drop which is caused by the plateclatiiode current of the amplifier pentode tube The plate-cathode current of tube VT4 changes depending on variations in the potential connected to the control grid of this tube. A varying grid potential is obtained from a point on a voltage divider bridge comprising resistors R1 and R3 connected between the +450-V and the O-V bus bars.

If the voltage on the bus bar designated +450-V should tend to rise, a proportion of the voltage difference between this point and 0 volts is impressed on the control grid of tube VT4 and results in an increased plate-cathode current and accordingly an increased voltage drop across the resistor R3. This increased voltage drop lowers the potential on the control grid of the regulator tube VT3 thereby reducing its plate output. The reduction in output is, of course, accomplished by an increase in the impedance between the plate and cathode of tube VT3, thus tending to lower the voltage on the +450-V bus bar. All of these actions to bring the output into regulation occur almost instantaneously.

In a similar manner a tendency of the voltage between the bus bars +450-Vv and O-V to decrease causes a decrease of the potential applied to the control grid of tube VT4 which results in a decrease in the plate-cathode current and accordingly 8, decreased voltage drop through resistor R3. This decreased voltage drop increases the potential on the control grid of the regulator tube VTlthereby increasing its plate current. Increase in output is accomplished by a decrease in the impedance between the plate and cathode of tube VT3 thus tending to raise the voltage on the +450-V bus bar. As stated previously, all of these actions take place almost instantaneously.

The Junction of the two resistors R9 and RIO bridged in series' between the +450-V and +150-V bus bars is connected to the filaments oi tubes VT3, VTl, VTIO and VTIE to keep the potentials of these tubes within the heater to cathode voltage requirement. Anti-sing resistors for parasitic suppression include the screen grid resistor RI and the grid resistor R2 associated with tube VT3.

For supplying voltage between the +150-V and O-V bus bars, a half wave rectifier tube VT2 is provided. A 400-volt, 400-cycle alternating current input to the tube is obtained from the lower half, of the secondary winding S0 of transformer TI and the filament is heated from the secondary The direct cur-. rent output from the plate of tube VT2 is smoothed by a double section filter comprising the series choke coils LIO and LII and the bridged condensers CH, CI5 and CIG. The rectified voltage output is reduced by the series resistor R4 and the output potential is fixed at 150 19' volts by the shunt regulator gas tube VTI. Condenser CII also absorbs any voltage surges which might be generated by gas tube VTI.

Nine circuits extending between the synchro step-by-step converter and the searchlight unit are required for controlling the azimuth and elevation motors I and ll! of the searchlight unit. These conductors include conductors I to l, inclusive, extending from the stator and rotor windings of the azimuth motor II. to

terminals on the connector block 422, thence over conductors of cable 8 and contacts of Jack 2" and plug 2" to armatures of relays 2H and 2| 2; include conductors I to I, inclusive, extending from the stator and rotor windings of the elevation motor I to terminals of the connector block 2, thence over conductors of cable I and contacts of Jack 2" and plug 201 to armatures of relays III and 2M and includes conductor which extends from the negative terminal of the power supply at receptacle 404 of the searchlight unit to a terminal on connector block 432 and thence" over a conductor of cable 3 and contacts of Jack 2" and plug 201 to conductor 2".

Relays 2H and 2|! each have one winding terminal connected to the negative power supply conductor 23! and have their other winding terminals connected to the lower front contact of relay 2", thelower armature of which latter relay is connected over a conductor of cable "3 and conductor 4 through the rotor winding of the azimuth motor III of the searchlight to the positive terminal of the power supply at receptacle Ill. Thus when relay 2" is operated relays 2H and 2 I3 become operated to connect the transmitters Ta and T: over conductors of cable a: and conductors I to I, inclusive, with the azimuth'and elevation motors I and II! of the Searchlight unit.

Relays H2 and 2 each have one winding terminal connected to the negative power supply conductor 23! and have their other winding terminals connected to the lower back contact of relay 2" and thence as traced to the positive power supply terminal at receptacle 4 so that when relay 2" is unoperated relays 2I2 and 2 become operated to connect the stator windings of the azimuth and elevation motors I and II! in circuit over the front contacts of such relays, over contacts of plug 2 and Jack 235 over conductors of cable 224 and con tacts of plug 328 and Jack 12! to terminals on connector block I2I at the searchlight control station and thence as previously traced to brushes of the transmitters AT and ET. The rotors of the motors H8 and II are connected over conductors 4 and I, over conductors of cable 483, contacts of Jack 2" and plug 201, contacts of plug 2 and Jack 2", conductors of cable 324, contacts of plug 226 and Jack 32! and terminals of connector block 32l at the searchlight control station and thence as traced over contacts of switch as when operate o segments of the transmitters AT and ET.

Relay 208 is operable in a circuit from 24-volt supply conductor 2|! through its winding in parallel with resistance 2" and over the back contact of relay 2 I 0 to the other supply conductor 2I'I. Thus when relay 2" is unoperated relay operates and in turn causes the operation of relays 2H and 2l3. Relay 2III is operable in a circuit extending from the negative power supply conductor 229pthrough its winding to the lunction point between resistors R", R" and R" and thence over the three circuits previously traced to the brushes of the transmitter AT at the searchlight control station whereupon when Operation of the system The apparatus illustrative of the invention having now been described in detail, the manner in which the invention functions will now be discussed. The target while beyond searchlight range is iirst tracked by the radar unit and during such tracking switch 2" at the searchlight control station is maintained in its open position whereby relay 2" at the synchro step-by-step converter is unoperated, relays 2", 2H and 2|! are operated and relays H2 and 2 are unoperated. As previously described, with relay 2" operated the input terminals III and I02 and III and I B2 of the azimuth and elevation servoamplifiers are associated with the phase detectors I244 and 42!: at the searchlight unit, and

the azimuth and elevation synchro transmitters AT]: and E'In are associated with the azimuth and elevation synchro receivers ARs and ERs. respectively, and with the phase detectors 424a and In. Y i

It it be assumed that the searchlight Is oriented in azimuth to a position corresponding to the azimuth orientation of the radar antenna. '400-cycle alternating current voltage applied to the rotor winding of the azimuth synchro transmltter ATn at the radar unit and impressed upon the stator windings of such transmitter will cause voltages to be applied over the conductors extending to the corresponding stator windings of the azimuth synchro receiver AR-a, but if the rotor winding of the receiver is assumed to be positioned in a synchronous position with respect to the rotor winding of the radar synchro transmitter A'lh, the sum of the voltages induced into the rotor winding of receiver Ans from its stator windings will be zero and the azimuth phase detector 424A will produce no error voltage. As a consequence the voltages applied from the phase detector over conductors I and I" to the input terminals Ill and I02 of the azimuth servo-amplifier will be equal and there will be no response by the servo-amplifier.

It will now be assumed that the radar antenna is rotated to a diflerent relative direction from that of the searchlight and that the rotor windings of the synchro transmitter AT: and synchro receiver ARs become displaced with respect to each other. This displacement causes the generation of an alternating current voltage in the circuit of the rotor winding of the receiver ARs which is impressed across the input terminals Ill' and "2 on the connector block 42! associated with the azimuth phase detector 424A. With cycle voltage applied through the windings of transformer T1 between the mid-tap of the resistance "I bridged across the input terminals "I and "2 and the mid-tap of resistance I bridged across the output terminals 1 and Ill; current will flow through the rectii'iers I" and 454 in parallel during each positive hali' cycle of the 60-cycle alternating current source and as a consequence the resistance of both the rectifiers will be reduced.

Dependent upon the phasing of the voltage applied to the input terminals "I and 452 from the synchro receiver ARs, positive voltage will be applied to either rectifier 455 or rectifier 450 at the same time that its resistance has been decreased and negative voltage will be applied to the other rectifier. As a consequence the resistance of one rectifier is further decreased and the resistance of the other rectifier is increased and positive voltage pulsating at a frequency 60 cycles per second will appear on either output terminal 451 or 450 and will be applied therefrom over the circuits previously traced in the input terminal IIII or terminal I02 of the azimuth servo-amplifier, and the negative voltage appearing on the other terminal of the pair 451 and 450 and applied therefrom to the other input terminal IOI or I02 oi the amplifier becomes less positive, or negative with respect to the voltage applied to the other terminal of the pair IOI', I02. The amplitude of this change in voltage depends upon the relative amount of the angular displacement between the rotors of the synchro transmitter ATn and the synchro receiver ARs and the polarity oi the voltage depends upon the direction 01' rotation producing the change.

This error voltage is registered at the searchlight unit, at the searchlight control station and at the radar unit by the deflection of the needles oi the azimuth zero-reader meters H0, 340 and 502, the windings of which are connected in parallel between the output terminals 451 and 450 at the azimuth phase detector 424A. The needles will remain deflected until the searchlight is rotated in azimuth to a position corresponding to the position assumed by the radar antenna.

The pulsating error voltages applied to the lnput terminals IM and I02 of the azimuth servoamplifier are. as previously described, filtered and amplified by the voltage amplifier tubes VTI and VT9, and the amplified voltages are applied to the control grids of the multivibrator tube VTI I. The outputs from the tube VIII are further amplified by the buffer or power amplifier tube VTI2 to cause the control relays AA and BA to operate and release in alternation at a frequency of approximately 40 cycles per second. The effect of these error voltages will be to cause the periods during which relay AA or relay BA is operated to be increased and to cause the periods during which the other of the relays is operated to be decreased. The lengths of time either relay remains operated while the other is released depends upon the polarity and amplitude of the error voltage.

The pair of relays vibrating in opposite phase, as above described, serves the dual purpose of rotating the motor MA and the transmitter TA driven thereby in a clockwise or a counter-clockwise direction as determined by the polarity of the error voltage and of rotating it at a speed proportional, for small values of voltages, to the amplitude of those voltages. The operating voltage connected across the armature of the motor MA.is related to the relative length of time the vibratory contacts of the relays are closed as compared to the length of time they are open. The greater the difference in the length of the opened and closed periods the greater will be the net voltage connected in one direction or the other across the armature of the'motor. This provides a variable speed control since the speed 01 the motor varies in proportion to the voltage connected across its armature.

With relay 2 I I operated as previously described the rotation of the brushes oi the transmitter TA transmits impulses through the stator windings of the azimuth motor I oi the searchlight unit and with the rotor circuit of the motor also established to the positive voltage segments of the transmitter TA through the operation oi. relay 2II, the motor 0 rotates in such a direction that it rotates the searchlight in a direction to direct the beam therefrom in azimuth towards the target which has been detected by the radar unit. As a consequence of such rotation the rotor of the synchro receiver ARs is rotated until, when the searchlight has reached an azimuth position corresponding to the azimuth position oi the radar antenna, such rotor winding will impress no error voltage upon the input terminals "I and 452 of the azimuth phase detector 424A and no error voltage will appear on the input terminals IN and I 02 of the azimuth servoamplifier. Therefore, the motor MA will come to rest and the transmitter TA will cease transmitting impulses to the motor H0 and the motor 4I0 will come to rest.

In a similar manner when the radar antenna is tilted in elevation to direct the radio beam on the target, the elevation synchro transmitter E'Ia, which is connected with the synchro receiver ERs, of the searchlight unit, will cause the generation of an error voltage across the input terminals 459 and 460 of the elevation phase detector 424a and will cause the generation of a pulsating voltage across the output terminals 46I and 452, the polarity of which will depend upon the direction of the rotation of the elevation transmitter ETn. producing the change and the amplitude of which will depend upon the relative amount of angular displacement. This pulsating error voltage is applied across the input terminals I 5| a'nd I52 of the elevation servo-amplifier and causes the servo-motor Me to drive the transmitter Tn in a direction dependent upon the polarity of the error voltage and at a speed dependent upon the amplitude of such voltage.

In response to the operation of the transmitter Tr: the elevation motor 4 I 9 of the searchlight unit causes the searchlight to be tilted in elevation until, when it has reached a tilted position corresponding to the elevation position of the radar antenna, the rotor winding of the elevation synchro receiver ERs, driven by the motor 4|, will be rotated to such a position that no error voltage will be impressed upon the input terminals 459 and 460 oi. the elevation phase detector 424s and no error voltage will appear across the input terminals I5I and I52 of the elevation servo-amplifier. Thereupon the motor Ma will come to rest and the transmitter Ta: will cease transmitting impulses to the motor 9 and the motor 4 I 9 will come to rest. Until the searchlight has been tilted in elevation to'a position in agreement with the tilting of the radar antenna the needles of the elevation zero-readermeters I, 4 and 503 will be deflected.

when the searchlight has thus been directed in azimuth and elevation into a position corresponding to the orientation of theradio beam on the target, the azimuth zero-reader meters 040, M0 and 502 and the elevation zero-reader meters I4I, 4H and 503 will read zero. When 7 the zero-reader meters are operated so that their 23 needles register zero, the accurate painting or the searchlight toward the target will be indicated.

When the target comes within searchlight range the operator at the searchlight unit will cause the arc in the searchlight lamp 3 to be struck by operating the arc switch 3. After the arc is struck the operator at the searchlight control station will slew the binoculars III by the operation of the azimuth hand wheel 32. and the operation of the elevation hand wheel (not shown) to coincide with the end of the searchlight beam. As soon as the target becomes visible to the operator he will operate the switch I. With switch 839 operated relay III in the synchro step-by-step converter becomes operated thereby releasing relay 2".

Relay 2" upon releasing short-circuits the inputs of the azimuth and elevation servo-amplitiers, releases relays 2H and ill and causes relays III and 2 to operate. Relays 1H and III upon releasing disconnect the transmittus Ta and T1: of the synchro step-by-step converter from the azimuth and elevation motors "l and II! of the searchlight unit. With the input terminals of the servo-amplifiers now short-circuited so that no error voltages may reach such amplitiers and the transmitters Ta and Ta disconnected, the radar unit has no further control of the searchlight unit. With relays Ill and Ill now operated the brushes oi the azimuth and elevation transmitters AT 'and E1 at the searchlight control station are connected over cmductors of cable 324, over contacts 01' such relays and conductors of cable "I with the azimuth and elevation motors H8 and ll. of the searchlight unit.

The operator at the searchlight control station may now operate the hand wheels of the station including the azimuth control wheel 32. and the elevation control wheel (not shown) to keep the binoculars 33! trained upon the target. The operation of such control wheels turns the brushes 0! the transmitters AT and E1 to trammit impulses to the motors I and I and such motors then turn the searchlight in azimuth and elevation directions to maintain the searchlight beam directed upon the target.

The radar is now tree'to search (or another target or to be associated with another searchlight and to direct such searchlight upon another target which may be tracked by such radar.

What is claimed is:

1. In a Searchlight control system, a searchlight, a motor of the step-by-step W for tuming said searchlight in azimuth, a radio dircction and range device for tracking a target, a synchro transmitter responsive to the tracking 01 said target in accordance with the azimuth direction of the radio beam, a synchro receiver at said searchlight operabl in accordance with the azimuth direction or the searchlight, means for connecting said synchro transmitter with said synchro receiver, means under the joint conh'ol 01 said synchros for generating an error voltage the polarity of which depends upon the direction of divergence between the positions of said synchros and the amplitude of which depends upon the amount of divergence, a servo-ampliiier responsive to said error voltage, a servomotor controlled by said amplifier, and a transmitter operable by said servo-motor for operating said searchlight turnin motor to bring the azimuth direction of said searchlight into cor respondence with the azimuth direction of the radio beam.

2. In a searchlight control system, a searchlight. a motor or the step-by-step type ior tilting said searchlight in elevation, a radio direction and range device for tracking a target, a synchrotransmitter responsive to the trackin 0i said target in accordance with the elevation direction of the radio beam, a synchro receiver at said searchlight operable in accordance with the elevation direction of the searchlight, means for connecting said synchro transmitter with said synchro receiver, means under the Joint control at said synchros for generating an error voltage the polarity of which depends upon the direction oi divergence between the positions of said synchros and the amplitude of which depends upon the amount of divergence, a servoampliiier responsive to said error voltage, a servomotor controlled by said amplifier and a transmitter operable by said servo-motor tor operating said searchlight tilting motor to bring the elevation direction 01 said searchlight into correspondence with the elevation direction of the radio beam.

3. In a searchlight control system, a searchiight, a motor of the step-by-step type for turning said 'searchiight in azimuth, a radio direction and range device for tracking a target, a synchro transmitter responsive to the tracking or said target in accordance with the azimuth direction of the radio beam, a synchro receiver at said searchlight operable in accordance with the azimuth direction 0! the Searchlight, "a searchlight control station, a transmitter at said station for controlling said motor, circuits for interconnecting said synchros, means under the Joint control of said synchros for generating an error voltage the polarity of which depends upon the direction of divergence between the positions of said synchros and the amplitude of which depends upon the amount of divergence, a servoampliiier responsive to said error voltage, a servomotor controlled by said amplifier, a transmitter operable by said servo-motor for operating said searchlight turning motor to bring the azimuth direction of said searchlight into correspondence with the azimuth direction of the radio beam, and relay means controllable from said station for removing the control of said turning motor irom said latter transmitter and for placing said turning motor under the control of said control station transmitter.

4. In a searchlight control system, a searchlight, a motor of the step-by-step type for turnins said searchlight in elevation, a radio direction andrange device for tracking a target, a synchro transmitter responsive to the tracking of said target in accordance with the elevation direction 0! the radio beam, a synchro receiver at said searchlight operable in accordance with the elevation direction of the Searchlight, a searchlight control station, a transmitter at said station for controlling said motor, circuits for interconnecting said synchros, means under the joint control 01' said synchros for generating an error voltage the polarity of which depends upon the direction of divergence between the positions of said synchros and the amplitude of which depends upon the amount of divergence, a servoampliiler responsive to said error voltage, a servo.- motor controlled by said amplifier, a transmitter operable by said servo-motor for operating said searchlight tilting motor to bring the elcvatfon direction of said Searchlight into correspondence with the elevation direction of the radio beam, and relay means controllable from said station for removing the control of said tilting motor Number from said latter transmitter and for placing said 2,075,083 tilting motor under the control 01' said control 2,257,757 station transmitter. 2,347,590 WILTON T. REA.- 2,376,359 2,399,426 REFERENCES CITED 1 2 417 24 The following references are of record in the tile of this patent: Number UNITED STATES PATENTS 555,052

Number Name Date 1,743,794 Murphy Jan. 14. 1930 Name Date Berna'rde Mar. 30, 1937 Moseley Oct. 7, 1941 Binder Apr. 25, 1944 Hultin May 22, 1945 Bradley Apr. 30, 1946 Godet Mar. 11, 1947 FOREIGN PATENTS Country Date Great Britain Aug. 3, 1943 

